VECTORDEFENCE DRONE
INTELLIGENCE
INDEPENDENT PERSPECTIVE
THE EVOLVING FIELD GUIDE
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DEFENCE DRONES / THE LIBRARY

Compare the evidence.

Choose up to three systems. Specifications retain their source and configuration; missing information is left undisclosed.

BirdEye 650D

Small tactical reconnaissance aircraft with fuel propulsion, a launcher and parachute recovery.

Country / region
Israel
Programme status
Order / production commitment
Sources reviewed
20 Sept 2026
Order / production commitmentOrder / production commitment
Primary domain
Air
System type
Reconnaissance aircraft
Developer / manufacturer
Israel Aerospace Industries
Origin / production countries
Israel
Other names
No additional names recorded
Variants / configurations
See the named configuration and evidence notes
Operators / programme customers
Customers not named in the reviewed production announcement

Evidence & current status

Public sources establish the programme and advertised configuration. Specifications are attributed claims, not independently certified performance.

Role & capabilities

  • Reconnaissance aircraft

Specifications in context

Airframe
Small fixed-wing tactical UAS

Manufacturer-published figure; configuration and conditions may affect performance.

Source ↗
Launch / recovery
Pneumatic launcher; parachute and airbag recovery

Manufacturer-published figure; configuration and conditions may affect performance.

Source ↗
Propulsion
Gasoline internal-combustion engine

Manufacturer-published figure; configuration and conditions may affect performance.

Source ↗
Dimensions
Wingspan 4 m

Manufacturer-published figure; configuration and conditions may affect performance.

Source ↗
Mass
Maximum take-off weight 30 kg

Manufacturer-published figure; configuration and conditions may affect performance.

Source ↗
Endurance
Up to 15 hours

Manufacturer-published figure; configuration and conditions may affect performance.

Source ↗
Range
150 km manufacturer operating range

Manufacturer-published figure; configuration and conditions may affect performance.

Source ↗
Speed
40 KTAS loiter; 80 KTAS maximum

Manufacturer-published figure; configuration and conditions may affect performance.

Source ↗
Altitude
15,000 ft AGL, as stated by manufacturer

Manufacturer-published figure; configuration and conditions may affect performance.

Source ↗
Payload
Maximum 5.5 kg

Manufacturer-published figure; configuration and conditions may affect performance.

Source ↗
Sensors
Stabilised day/night imaging payload

Manufacturer-published figure; configuration and conditions may affect performance.

Source ↗
Communications / navigation
Not established from the reviewed public sources.

Public data gap; no estimate or neighbouring variant value substituted.

Source ↗